
Embraer Prodigy® Flight Deck 100 Pilot’s Guide
190-00728-04 Rev. A
460
AUTOMATIC FLIGHT CONTROL SYSTEM
CHANGING THE AIRSPEED REFERENCE (FLC MODE)
TheAirspeedReference(shownabovetheAirspeedIndicator)maybeadjustedby:
•Usingthe
SPD SEL
Knob
•Pressingthe
CWS
Button, hand-flying the aircraft to attain a new Airspeed Reference, then releasing the
CWS
Button
Duringclimb,theAirspeedReferenceunitsautomaticallychangefromIAStoMachwheneitherthealtitude
ortheairspeedlistedin Table7-3areattained.Fordescent, theunitsswitchbackat thespeciedaltitude
or airspeed. The system determines aircraft climb or descent by the relationship between the current and
Selected altitudes.
Airspeed Reference Units Unit Type Changes At:
Default Units Change To: Altitude Airspeed
Climb IAS Mach > 31,500 ft > M 0.55
Descent Mach IAS < 30,500 ft < 250 kt
Table 7-3 FLC Mode Unit Changes
AirspeedReferenceunitscanbemanuallytoggledbetweenIASand MachunitsbypressingtheSPD SEL
Knob.When theFLC AirspeedReference isdisplayedin Mach,the AirspeedReferenceBug isdisplayed
ontheAirspeedIndicatorattheIAScorrespondingto theselectedMachtargetspeedandthecurrentMach
numberisshownbelowtheAirspeedIndicator.
Figure 7-12 Flight Level Change Mode (Mach)
Airspeed
Reference
Bug
Airspeed
Reference
(Mach)
Selected Altitude
Capture Mode Armed
Flight Level Change
Mode Active
Command Bars Indicate Climb
to attain Selected Altitude
TheAirspeedReferenceBugcan besetatalltimes (tobeusedasa visualreference)exceptwhenCSC is
engaged.InCSCmodetheAirspeedReferenceBugisxedandsetattheairspeedexistingatthetimeofCSC
engagement.Whilethebug canbesetduringthese modesitisonlybeing controlledwheninFLCmode,
when CSC is engaged, etc.